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SAE technical paper series, Volume 730364.
Impacts of mission-related requirements on design of the J402-CA-400 missile propulsion turbojet engine are reviewed. Small-engine cost scaling rationale is... 
Military aircraft | Turbojet engines
eJournal
SAE technical paper series, Volume 2005-01-3379.
This paper presents an overview of two long-range supersonic cruise missile prototypes and the preliminary design of the Missile Control System (MCS). The MCS... 
Design processes | Missiles | Electronic control systems | Turbojet engines
eJournal
1990, Progress in astronautics and aeronautics : an American Institute of Aeronautics and Astronautics series, ISBN 9780930403683, Volume 124., xv, 341
Book
SAE technical paper series, Volume 871480.
The development of a portable liquid cooling system for a missile seeker section is described. The unique element of the cooling system is a flexible cooling... 
Missiles | Test equipment and instrumentation | Engine cooling systems
eJournal
1996, Progress in astronautics and aeronautics, ISBN 9781563471186, Volume 170, xv, 529
Book
SAE technical paper series, Volume 941200.
This paper illustrates the growing commonality between aircraft structural requirements for materials and the need for similar materials in systems installed... 
Missiles | Rocket engines
eJournal
SAE technical paper series, Volume 2006-01-3099.
A very high power source solution was developed for the Non Line of Sight Launch System Container Launch Unit (NLOS-LS CLU). The power source solution has been... 
Missiles | Product development | Energy storage systems | Engines
eJournal
SAE technical paper series, Volume 580167.
ABSTRACT The application of the turbine engine to high flight speed missiles is considered and the advantages that such missiles have are discussed. In order... 
Missiles | Turbojet engines
eBook
Nuclear Engineering and Design, ISSN 0029-5493, 08/2018, Volume 335, pp. 44 - 53
The aircraft collision with RC structures would lead to the global response and local damage, which are mainly caused by the impact of the entire aircraft and... 
RC panel | Nuclear power plant (NPP) containment | Aircraft impact | Engine | Penetration depth | CONTAINMENT | BEHAVIOR | SIMULATION | REINFORCED-CONCRETE SLABS | LOCAL DAMAGE | SOLID MISSILES | CRASH | COMMERCIAL AIRCRAFT | FORCE | NUCLEAR SCIENCE & TECHNOLOGY | NUCLEAR-POWER-PLANT | Guided missiles | Rockets (Ordnance) | Nuclear energy | Nuclear power plants | Aircraft engines
Journal Article
SAE technical paper series, Volume 2003-01-3064.
In recognition of the centennial of manned flight, this perspective on more than 100 years of unmanned flight details some of the major developments in the use... 
Missiles | Radio equipment | Military aircraft | Electric vehicles | Engines
eJournal
International Journal of Impact Engineering, ISSN 0734-743X, 01/2015, Volume 75, pp. 75 - 87
This paper presents a three-step method for designing steel plate composite (SC) walls subjected to missile impact. This method can be used to compute the... 
Projectile impact | Concrete | Steel plate | Composite structure | SPHERICAL-NOSE RODS | REINFORCED-CONCRETE | PENETRATION | PLATES | ENGINEERING, MECHANICAL | LOCAL DAMAGE | AIRCRAFT ENGINE MISSILES | PROJECTILES | MECHANICS | TARGETS | SHEAR CONNECTORS | Guided missiles | Rockets (Ordnance) | Analysis | Missiles | Databases | Perforation | Mathematical analysis | Benchmarking | Mathematical models | Steels | Walls
Journal Article
Journal of Spacecraft and Rockets, ISSN 0022-4650, 07/2017, Volume 54, Issue 4, pp. 930 - 935
Journal Article
Nuclear Engineering and Design, ISSN 0029-5493, 2010, Volume 240, Issue 10, pp. 2633 - 2642
▶ Experimental series on UHPC panels subjected to aircraft engine impact. ▶ Improved ballistic limit of fiber reinforced UHPC in comparison to conventional... 
NUCLEAR SCIENCE & TECHNOLOGY | REINFORCED-CONCRETE | Analysis | Aircraft engines
Journal Article
Propellants, Explosives, Pyrotechnics, ISSN 0721-3115, 12/2018, Volume 43, Issue 12, pp. 1277 - 1286
Journal Article
Journal of Spacecraft and Rockets, ISSN 0022-4650, 07/2010, Volume 47, Issue 4, pp. 694 - 700
Journal Article
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